The Shock and Vibration Bulletin.
Abstract
;Contents: Reduction of vibrations in aerospace structures by additive damping; Vibration isolation with nonlinear damping; The control of vibrations with viscoelastic materials; Sonic fatigue resistance of structures incorporating a constrained viscoelastic core; Experiments of inelastic damping of space vehicle ducts; Transverse vibrations of laminated plates with viscoelastic layer damping; Comparison of the geiger thick plate test and the vibrating composite beam test for the evaluation of the effectiveness of vibration damping materials; An aerospace energy absorber applied to highway safety; Determination of the complex mobility and impedance matrices for damped lumped parameter linear dynamic systems; 'Wagging tail' vibration absorber; A simple device for attenuation of longitudinal elastic stress waves; Analysis of shock mitigation for glass submersibles; Reduction in vibration of the CH-47C helicopter using a variable tuning vibration absorber; Response and optimization of an isolation system with relaxation type damping; The response of mechanical shock isolation elements to high rate input loading; Rational analysis of a two-degree-of-freedom flexure-torsion system; Design and development of a shock isolation evaluation system; A study of amplitude frequency plots with nonlinear damping; Vibrations of multicore sandwich beams; The use of polyurethane foam for shock and vibration isolation of avionics components; The analytic modeling of open-cell foams as shock and vibration elements.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1969
- Accession Number
- AD0723344